SE9101038L - SUBSTRATE PART ORGANIZED TO BE SEPARATED FROM AN AIRCRAFT - Google Patents
SUBSTRATE PART ORGANIZED TO BE SEPARATED FROM AN AIRCRAFTInfo
- Publication number
- SE9101038L SE9101038L SE9101038A SE9101038A SE9101038L SE 9101038 L SE9101038 L SE 9101038L SE 9101038 A SE9101038 A SE 9101038A SE 9101038 A SE9101038 A SE 9101038A SE 9101038 L SE9101038 L SE 9101038L
- Authority
- SE
- Sweden
- Prior art keywords
- sub
- combat unit
- carrier
- target area
- separated
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/50—Brake flaps, e.g. inflatable
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A sub-combat unit arranged to be separated from a flying body, for example a carrier shell or the like, over a target area, the sub-combat unit comprising a warhead (4), a target detector (5) and two diametrically disposed carrier surfaces (1,2) which impart to the sub-combat unit a rotation for scanning of the target area in a helical pattern during the fall of the sub-combat unit down towards the target area, the two carrier surfaces (1,2) being pivotally arranged from a closed position to an opened position in which the two carrier surfaces (1,2) form a retarding area for the fall velocity of the sub-combat unit. At least one of the two carrier surfaces (1,2) includes devices (9,10) to achieve so-called relieved flow of the carrier surface for different angles of wind impingement (8) in relation to the carrier surface (2). The said devices may comprise for example a wing-like flap (9), an angled portion (11) or a hole (10) in the vicinity of one end of the carrier surface (2). By this means a uniform and stable scanning movement on the part of the sub-combat unit is obtained. <IMAGE>
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9101038A SE468262B (en) | 1991-04-08 | 1991-04-08 | SUBSTRATE PART ORGANIZED TO BE SEPARATED FROM AN AIRCRAFT |
EP92850218A EP0587970B1 (en) | 1991-04-08 | 1992-09-14 | Sub-combat unit |
US07/957,487 US5282422A (en) | 1991-04-08 | 1992-10-07 | Sub-combat unit |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9101038A SE468262B (en) | 1991-04-08 | 1991-04-08 | SUBSTRATE PART ORGANIZED TO BE SEPARATED FROM AN AIRCRAFT |
EP92850218A EP0587970B1 (en) | 1991-04-08 | 1992-09-14 | Sub-combat unit |
Publications (2)
Publication Number | Publication Date |
---|---|
SE9101038L true SE9101038L (en) | 1992-10-09 |
SE468262B SE468262B (en) | 1992-11-30 |
Family
ID=26132596
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE9101038A SE468262B (en) | 1991-04-08 | 1991-04-08 | SUBSTRATE PART ORGANIZED TO BE SEPARATED FROM AN AIRCRAFT |
Country Status (3)
Country | Link |
---|---|
US (1) | US5282422A (en) |
EP (1) | EP0587970B1 (en) |
SE (1) | SE468262B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE501082C2 (en) * | 1993-03-30 | 1994-11-07 | Bofors Ab | Method and apparatus for giving an airborne combat section a desired pattern of movement |
SE505189C2 (en) * | 1994-11-16 | 1997-07-14 | Bofors Ab | Methods and apparatus for combating combat elements along the route of the carrier's vehicle released from a carrier vehicle |
FR2769287B1 (en) | 1997-10-08 | 1999-12-24 | Lacroix Soc E | DEVICE FOR BRAKING A FALL OF A LOAD |
AUPR303501A0 (en) * | 2001-02-09 | 2001-03-08 | Kusic, Tom | Spiralling missile |
SE536255C2 (en) * | 2012-02-06 | 2013-07-23 | Bae Systems Bofors Ab | Brake panel for a spark plug or projectile |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1626363A (en) * | 1921-10-14 | 1927-04-26 | Elmer A Sperry | Gravity bomb |
US2446279A (en) * | 1942-09-19 | 1948-08-03 | Rca Corp | Aerial bomb control system |
US2520665A (en) * | 1946-01-07 | 1950-08-29 | Bertram E Warren | Gyroscope control device for bombs |
NL186136B (en) * | 1953-04-23 | Kendall & Co | NON-WOVEN TEXTILE MATERIAL SUITABLE FOR USE AS A MEDICAL BANDING. | |
DE2538665A1 (en) * | 1975-08-30 | 1977-03-10 | Messerschmitt Boelkow Blohm | PROCEDURE AND EQUIPMENT FOR LETTERING BOMBS |
US4004514A (en) * | 1976-01-20 | 1977-01-25 | The United States Of America As Represented By The Secretary Of The Navy | Roll rate stabilized wrap around missile fins |
US4492166A (en) * | 1977-04-28 | 1985-01-08 | Martin Marietta Corporation | Submunition having terminal trajectory correction |
SE452505B (en) * | 1986-03-27 | 1987-11-30 | Bofors Ab | SUBSCRIPTION PART WITH SWINGABLE MOLD DETECTOR |
SE461750B (en) * | 1987-03-20 | 1990-03-19 | Lars Johan Schleimann Jensen | PROCEDURES FOR CONTROL OF A FLYING OBJECT, SUCH AS A PROJECT, AGAINST A TARGET AND PROJECT FOR THE IMPLEMENTATION OF THE PROCEDURE |
USH685H (en) * | 1988-06-20 | 1989-10-03 | The United States Of America As Represented By The Secretary Of The Army | Deployable fin configuration for free flight control of cylindrical bodies |
SE464834B (en) * | 1989-10-20 | 1991-06-17 | Bofors Ab | SUBSCRIPTION PART WITH SWINGABLE BEAR SURFACES |
SE464833B (en) * | 1989-10-20 | 1991-06-17 | Bofors Ab | SUBSCRIPTION PART WITH SWINGABLY ORGANIZED MEAL DETECTOR AND BARE AREA |
SE465440B (en) * | 1990-04-04 | 1991-09-09 | Bofors Ab | submunition |
US5067410A (en) * | 1990-12-21 | 1991-11-26 | The United States Of America As Represented By The Secretary Of The Army | Flexible wing |
-
1991
- 1991-04-08 SE SE9101038A patent/SE468262B/en not_active IP Right Cessation
-
1992
- 1992-09-14 EP EP92850218A patent/EP0587970B1/en not_active Expired - Lifetime
- 1992-10-07 US US07/957,487 patent/US5282422A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US5282422A (en) | 1994-02-01 |
SE468262B (en) | 1992-11-30 |
EP0587970B1 (en) | 1998-12-09 |
EP0587970A1 (en) | 1994-03-23 |
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